Test of NACA model 11-C with angle of afterbody keel at five different settings from 2 1/2 to 9°; effect of variation of angle of afterbody keel upon take-off performance.


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    Title :

    Effect of angle of afterbody keel on water performance of flying-boat Hull model


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:


    Publication date :

    1935


    Size :

    10 pages


    Remarks:

    36 Supp Sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :